Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/22133
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dc.contributor.authorKulik M.S.-
dc.contributor.authorAntonov V.K.-
dc.contributor.authorGlazok O.M.-
dc.contributor.authorOlefir O.I.-
dc.contributor.authorГлазок, Олексій Михайлович-
dc.contributor.authorГлазок О.М.-
dc.contributor.authorГлазок, Алексей Михайлович-
dc.contributor.authorГлазок А.М.-
dc.date.accessioned2016-08-02T13:22:31Z-
dc.date.available2016-08-02T13:22:31Z-
dc.date.issued2015-10-
dc.identifier.citationUnmanned aircraft with a closed wing /M.S.Kulik, V.K.Antonov, O.M.Glazok, O.I.Olefir //Proceedings of the 2015 IEEE 3rd International Conference "Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD)" October 13-15, 2015. Kyiv, Ukraine. – Pp. 54-58.en
dc.identifier.isbn978-1-4673-6566-6-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/22133-
dc.description.abstractA configuration of an unmanned aircraft with closed wing is considered. The method of identification designed for researching the aerodynamic qualities of the model is proposed.en
dc.description.urihttp://ieeexplore.ieee.org/xpl/login.jsp?tp=&arnumber=7346558&url=http%3A%2F%2Fieeexplore.ieee.org%2Fxpls%2Ficp.jsp%3Farnumber%3D7346558en
dc.language.isoenen
dc.publisherIEEEen
dc.subjectunmanned aircraften
dc.subjectclosed wingen
dc.subjectautomatic controlen
dc.subjectidentificationen
dc.subjectauxiliary equationen
dc.subjectsimulatoren
dc.titleUnmanned aircraft with a closed wingen
dc.typeThesisen
Appears in Collections:Матеріали конференції «Інтелектуальні технології лінгвістичного аналізу»



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